Unlock instant, AI-driven research and patent intelligence for your innovation.

Electronic Means for Detecting Buffered Main Shaft Seal Wear or Failure in a Turbine Engine

a turbine engine and main shaft seal technology, applied in the field of electronic means for detecting the wear or failure of the main shaft seal in the early detection field of gas turbine engines

Active Publication Date: 2013-10-24
RAYTHEON TECH CORP +1
View PDF3 Cites 23 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The present invention relates to a gas turbine engine with a bearing chamber leak detection system. The system includes a plenum between the bearing chamber and the surrounding walls, and a sensor to measure the airflow from the plenum into the chamber. The method involves measuring the flow of pressurized air into the chamber and comparing it to an expected value to detect any leaks in the chamber seals. This can prevent damage to the engine caused by unnoticed leaks and allow for timely repairs. The controller can also execute steps to measure the flow of pressurized air and compare it to an expected value to detect any leaks.

Problems solved by technology

A leak is determined to exist when the measured flow of pressurized air exceeds an expected flow of pressurized air.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Electronic Means for Detecting Buffered Main Shaft Seal Wear or Failure in a Turbine Engine
  • Electronic Means for Detecting Buffered Main Shaft Seal Wear or Failure in a Turbine Engine
  • Electronic Means for Detecting Buffered Main Shaft Seal Wear or Failure in a Turbine Engine

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0014]The present disclosure provides a system and method for the early and automatic detection of worn or damaged bearing chamber seals through the monitoring of the buffer system air flow. Before discussing the details of the improved leak detection system, the application environment will be briefly discussed in order to provide context for the reader. While the example application environment includes a turbofan gas turbine engine, it will be appreciated that this engine may be used in a land-based application such as at a generator station, or may be used in an air or other application, e.g., for propulsion of an aircraft. This disclosure also relates to the detection of failures in other air system components including but not limited to active clearance systems, buffer cooler systems, and other air systems both internal (tubes or passages) and external to the engine.

[0015]Referring now to FIG. 1, this figure shows a simplified schematic cross-section view of a turbofan gas tu...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

In accordance with an embodiment, a gas turbine engine is provided having a bearing chamber leak detection system. The gas turbine engine includes a rotatable shaft, a bearing assembly supporting the rotatable shaft, and a plurality of bearing chamber seals surrounding the rotatable shaft creating an annular bearing chamber enclosing the bearing assembly. One or more walls substantially surrounding the bearing chamber create a plenum between the walls and the bearing chamber, and a pressurized air inlet to the plenum is provided. The pressurized air inlet includes an airflow sensor configured and positioned to sense a flow of pressurized air into the plenum, such that airflow at the sensor is indicative of airflow from the plenum into the bearing chamber via one or more of the plurality of bearing chamber seals.

Description

TECHNICAL FIELD OF THE DISCLOSURE[0001]The present disclosure relates to gas turbine engines and, more particularly, relates to early detection of main shaft seal wear or failure.BACKGROUND OF THE DISCLOSURE[0002]The main shaft in a gas turbine engine is supported by one or more sets of bearings. While these bearings must be lubricated to ensure continuous and efficient operation of the engine, it is also desirable to minimize the extent to which the bearing chamber may leak lubricant. Not only can leaked lubricant potentially contaminate nearby systems, but undetected leakage can also eventually lead to engine failure or damage. In addition to oil leakage, any leakage of high-temperature air into the bearing chamber could severely damage the bearings and compromise engine operation.[0003]Bearing chamber pressurization is often used in gas turbine engines (including ground based generator and derivatives thereof) to improve the effectiveness of the bearing chamber seals to maintain ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): F01D25/18G01M3/04
CPCF01D25/18G01M3/2869G01M15/14
Inventor PARNIN, FRANCISAMADOR, ARMANDO
Owner RAYTHEON TECH CORP